Validation of an Acoustically 3-D-Designed Turbine Exit Guide Vane-Reference-Cited by-同舟云学术

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Validation of an Acoustically 3-D-Designed Turbine Exit Guide Vane

Published:2010-06-07 Issue: Volume: Page:
ISSN:
Container-title:16th AIAA/CEAS Aeroacoustics Conference
language:
Short-container-title:

Author:

Broszat Dominik¹,Kennepohl Fritz¹,Tapken Ulf²,Moser Mathias³,Heitmeir Franz³

Affiliation:

1. MTU Aero Engines GmbH

2. German Aerospace Center (DLR)

3. Graz University of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-3806

Reference8 articles.

1. 2Broszat, D., Korte, D., Tapken, U., and Moser, M. “Validation of Turbine Noise Prediction Tools with Acoustic Rig Measurements,” AIAA-2009-3283.

2. DESIGN SELECTION AND ANALYSIS OF A SWEPT AND LEANED STATOR CONCEPT

3. Passive Noise Control by Blade Lean and Sweep

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Acoustic Comparison of Different Turbine Exit Guide Vane Designs - Part 1: Design Philosophy and Numerical Predictions;21st AIAA/CEAS Aeroacoustics Conference;2015-06-18

2. On the Influence of Rotor Design on an Acoustically 3d-Designed Turbine Exit Guide Vane;20th AIAA/CEAS Aeroacoustics Conference;2014-06-13

3. Verification of the Inverse Cut-off Effect in a Turbomachinery Stage - Part 1 - Numerical results;18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference);2012-06-04

4. Validation of an Integrated Acoustic Absorber in a Turbine Exit Guide Vane;17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference);2011-06-05

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